FR2537916B1 - Procede de realisation d'elements de construction a partir de couches de matiere plastique renforcee de fibres - Google Patents
Procede de realisation d'elements de construction a partir de couches de matiere plastique renforcee de fibresInfo
- Publication number
- FR2537916B1 FR2537916B1 FR8319955A FR8319955A FR2537916B1 FR 2537916 B1 FR2537916 B1 FR 2537916B1 FR 8319955 A FR8319955 A FR 8319955A FR 8319955 A FR8319955 A FR 8319955A FR 2537916 B1 FR2537916 B1 FR 2537916B1
- Authority
- FR
- France
- Prior art keywords
- layers
- plastic material
- fiber reinforced
- reinforced plastic
- construction elements
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/06—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/002—Inorganic yarns or filaments
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/002—Inorganic yarns or filaments
- D04H3/004—Glass yarns or filaments
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
- D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
- D04H3/105—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by needling
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
- D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
- D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
- D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
- D04H3/115—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by applying or inserting filamentary binding elements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
- B29C65/564—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined hidden in the joint, e.g. dowels or Z-pins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
- B29C66/3034—Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes
- B29C66/30341—Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes non-integral with the parts to be joined, e.g. making use of extra elements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/45—Joining of substantially the whole surface of the articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
- B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/07—Parts immersed or impregnated in a matrix
- B32B2305/076—Prepregs
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249923—Including interlaminar mechanical fastener
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/60—Nonwoven fabric [i.e., nonwoven strand or fiber material]
- Y10T442/654—Including a free metal or alloy constituent
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Inorganic Chemistry (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19823246803 DE3246803A1 (de) | 1982-12-17 | 1982-12-17 | Verfahren zum herstellen von bauteilen aus lagen von faserverstaerktem kunststoff |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2537916A1 FR2537916A1 (fr) | 1984-06-22 |
FR2537916B1 true FR2537916B1 (fr) | 1987-02-20 |
Family
ID=6180989
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8319955A Expired FR2537916B1 (fr) | 1982-12-17 | 1983-12-13 | Procede de realisation d'elements de construction a partir de couches de matiere plastique renforcee de fibres |
Country Status (5)
Country | Link |
---|---|
US (1) | US4528051A (es) |
DE (1) | DE3246803A1 (es) |
ES (1) | ES8505583A1 (es) |
FR (1) | FR2537916B1 (es) |
GB (1) | GB2132134B (es) |
Families Citing this family (54)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3302337C2 (de) * | 1983-01-25 | 1986-08-07 | Deutsche Fibrit Gesellschaft Ebers & Dr. Müller mbH, 4150 Krefeld | Verfahren und Vorrichtung zum Kaschieren von Verkleidungen |
US4740257A (en) * | 1985-03-04 | 1988-04-26 | Acoustic Industries, Inc. | Ceiling tile covering system |
GB8618727D0 (en) * | 1986-07-31 | 1986-09-10 | Wiggins Teape Group Ltd | Thermoplastic sheets |
US4808461A (en) * | 1987-12-14 | 1989-02-28 | Foster-Miller, Inc. | Composite structure reinforcement |
GB8927734D0 (en) * | 1989-12-07 | 1990-02-07 | Short Brothers Plc | A composite material |
US5186776A (en) * | 1990-05-07 | 1993-02-16 | Foster-Miller, Inc. | Composite laminate translaminar reinforcement apparatus and method |
GB9014770D0 (en) * | 1990-07-03 | 1990-08-22 | Short Brothers Plc | Manufacture of a composite material |
DE4030989A1 (de) * | 1990-10-01 | 1992-04-09 | Airbus Gmbh | Verfahren und vorrichtung zum verstaerken von bauteilen aus lagen von faserverstaerktem thermoplastischem kunststoff |
FR2687389B1 (fr) * | 1992-02-17 | 1994-05-06 | Aerospatiale Ste Nationale Indle | Dispositif et procede pour realiser une piece de structure complexe par depose au contact de fil ou ruban. |
US5466506A (en) * | 1992-10-27 | 1995-11-14 | Foster-Miller, Inc. | Translaminar reinforcement system for Z-direction reinforcement of a fiber matrix structure |
WO1994025178A1 (en) * | 1993-04-30 | 1994-11-10 | Foster-Miller, Inc. | A reinforced joint for composite structures and method of joining composite parts |
DE69434917T2 (de) * | 1993-05-04 | 2007-11-08 | Foster-Miller, Inc., Waltham | Gittergestützte verbundplatte mit schaumkern |
ATE164112T1 (de) * | 1993-09-25 | 1998-04-15 | Symalit Ag | Faserverstärkte, thermoplastische platte |
WO1995011797A1 (en) * | 1993-10-29 | 1995-05-04 | Foster-Miller, Inc. | Translaminar reinforcement system for z-direction reinforcement of a fiber matrix structure |
EP0748280A1 (en) * | 1994-01-24 | 1996-12-18 | Chemfab Corporation | Composites of fluoropolymers with thermally non-adherent non-fluoropolymers and methods for producing the same |
US5720143A (en) * | 1994-03-01 | 1998-02-24 | The United States Of America As Represented By The Secretary Of Agriculture | Localized notch reinforcement for wooden beams |
US5756973A (en) * | 1995-06-07 | 1998-05-26 | The Boeing Company | Barbed susceptor for improviing pulloff strength in welded thermoplastic composite structures |
WO1997039886A1 (fr) * | 1996-04-19 | 1997-10-30 | Gennady Ashotovich Amiryants | Panneau elastomere arme et cellule |
US5980665A (en) * | 1996-05-31 | 1999-11-09 | The Boeing Company | Z-pin reinforced bonds for connecting composite structures |
US5876540A (en) * | 1996-05-31 | 1999-03-02 | The Boeing Company | Joining composites using Z-pinned precured strips |
US5759924A (en) * | 1996-10-18 | 1998-06-02 | Chemfab Corporation | Translucent polymeric composite for use in an architectural load-bearing structure |
US6051089A (en) * | 1997-02-07 | 2000-04-18 | Mcdonnell Douglas Corporation | Reinforcing member for composite workpieces and associated methods |
US6291049B1 (en) | 1998-10-20 | 2001-09-18 | Aztex, Inc. | Sandwich structure and method of making same |
DE19935518A1 (de) * | 1999-07-28 | 2001-02-01 | Bayerische Motoren Werke Ag | Verbundteil mit übereinander angeordneten Schichten |
US6267175B1 (en) * | 2000-02-08 | 2001-07-31 | Honeywell International Inc. | Composite heat exchanger having strengthened joints |
US7105071B2 (en) * | 2001-04-06 | 2006-09-12 | Ebert Composites Corporation | Method of inserting z-axis reinforcing fibers into a composite laminate |
US6645333B2 (en) | 2001-04-06 | 2003-11-11 | Ebert Composites Corporation | Method of inserting z-axis reinforcing fibers into a composite laminate |
US7785693B2 (en) | 2001-04-06 | 2010-08-31 | Ebert Composites Corporation | Composite laminate structure |
US7731046B2 (en) * | 2001-04-06 | 2010-06-08 | Ebert Composites Corporation | Composite sandwich panel and method of making same |
US7056576B2 (en) * | 2001-04-06 | 2006-06-06 | Ebert Composites, Inc. | 3D fiber elements with high moment of inertia characteristics in composite sandwich laminates |
US20050025948A1 (en) * | 2001-04-06 | 2005-02-03 | Johnson David W. | Composite laminate reinforced with curvilinear 3-D fiber and method of making the same |
US6676785B2 (en) * | 2001-04-06 | 2004-01-13 | Ebert Composites Corporation | Method of clinching the top and bottom ends of Z-axis fibers into the respective top and bottom surfaces of a composite laminate |
US20050118448A1 (en) * | 2002-12-05 | 2005-06-02 | Olin Corporation, A Corporation Of The Commonwealth Of Virginia | Laser ablation resistant copper foil |
DE102005012496B3 (de) * | 2005-03-16 | 2006-10-26 | Technische Universität Berlin | Vorrichtung mit einem auf einem Montageteil montierten elektronischen Bauteil und Verfahren |
DE102005035681A1 (de) * | 2005-07-27 | 2007-02-08 | Röhm Gmbh | Fertigungsverfahren zur Armierung von Kernmaterialien für Kernverbunde sowie von Kernverbund-Strukturen |
US8709584B2 (en) * | 2006-01-31 | 2014-04-29 | Sikorsky Aircraft Corporation | Composite aircraft floor system |
US20100021682A1 (en) * | 2008-07-25 | 2010-01-28 | Florida State University Research Foundation | Composite material and method for increasing z-axis thermal conductivity of composite sheet material |
DE102008043314B4 (de) | 2008-10-30 | 2010-12-09 | Airbus Deutschland Gmbh | Verfahren und Vorrichtung zum Verstärken eines Substrats oder eines Textils einer Kernstruktur eines Bauelementes, beispielsweise eines Luft- oder Raumfahrzeugs |
WO2010058196A1 (en) * | 2008-11-19 | 2010-05-27 | Bae Systems Plc | Fibre reinforced composite |
DE102009010292A1 (de) * | 2009-02-24 | 2010-08-26 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung eines faserverstärkten Kunststoffbauteils |
JP5901518B2 (ja) * | 2009-06-12 | 2016-04-13 | クイックステップ、テクノロジーズ、プロプライエタリ、リミテッドQuickstep Technologies Pty,Ltd. | 高度複合構成要素の製造方法 |
DE102009047671A1 (de) * | 2009-12-08 | 2011-06-09 | Airbus Operations Gmbh | Verfahren zum Anbinden eines Faserverbundbauteils an ein Strukturbauteil eines Luft- und Raumfahrzeuges und eine entsprechende Anordnung |
FR2959442B1 (fr) * | 2010-04-30 | 2012-09-28 | Eads Europ Aeronautic Defence | Procede et dispositif d'assemblage de preformes en composites thermoplastiques |
DE102011101456A1 (de) * | 2011-05-13 | 2012-11-15 | Airbus Operations Gmbh | Verbindungsvorrichtung, Baugruppe und Verfahren zur Herstellung einer Baugruppe |
DE102011115406A1 (de) * | 2011-10-06 | 2013-04-11 | Airbus Operations Gmbh | Verfahren zum Verbinden von faserverstärkten Zwischenprodukten und Strukturbauteil mit faserverstärkten Zwischenprodukten sowie Verfahren und Vorrichtung zur Herstellung einer Adhäsionsschicht |
GB201117467D0 (en) | 2011-10-11 | 2011-11-23 | Rolls Royce Plc | A method of providing through-thickness reinforcement of a laminated material |
FR2998210B1 (fr) * | 2012-11-20 | 2017-03-10 | Plastic Omnium Cie | Ensemble d'un insert metallique et d'une nappe de materiau composite, procede d'incorporation d'un tel insert dans une telle nappe et piece obtenue par moulage d'une telle nappe |
JP6286022B2 (ja) | 2013-03-15 | 2018-02-28 | セリフォージ インコーポレイテッド | 複合材プリフォームの三次元製織方法及び漸変断面トポロジーを備えた製品 |
DE102014209815A1 (de) * | 2014-03-07 | 2015-09-10 | Leichtbau-Zentrum Sachsen Gmbh | Verfahren zur Verbindung von faserverstärkten Kunststoffbauteilen mit duroplastischer Matrix |
EP3034278B1 (de) * | 2014-12-19 | 2020-02-12 | Airbus Defence and Space GmbH | Bauteil mit stoffschlüssiger Verbindung und ein Fügeverfahren |
EP3034276B1 (de) | 2014-12-19 | 2021-06-30 | Airbus Defence and Space GmbH | Bauteil mit stoffschlüssiger Verbindung und ein Fügeverfahren |
EP3433100B1 (en) | 2016-03-21 | 2022-05-04 | Saint-Gobain Performance Plastics Corporation | Architectural membrane |
US10543646B2 (en) | 2018-01-12 | 2020-01-28 | Arevo, Inc. | Structural sewing and overmolding |
US11549391B2 (en) * | 2021-03-22 | 2023-01-10 | General Electric Company | Component formed from hybrid material |
Family Cites Families (18)
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US1657979A (en) * | 1926-05-03 | 1928-01-31 | Thomas Frederick William | Roofing material |
FR950104A (fr) * | 1943-01-30 | 1949-09-19 | Procédé de fixation d'éléments d'assemblage | |
GB891121A (en) * | 1957-05-07 | 1962-03-14 | Dracone Developments Ltd | Improvements in or relating to flexible barges or storage vessels |
US3451884A (en) * | 1964-08-05 | 1969-06-24 | Mitsubishi Petrochemical Co | Waterproof pile coated sheet for laminating |
US3464348A (en) * | 1967-06-02 | 1969-09-02 | Arthur E Mcglinchey | Apparatus for fabricating wooden structures |
GB1310355A (en) * | 1969-07-03 | 1973-03-21 | Foseco Trading Ag | Fibre containing compositions |
GB1244893A (en) * | 1969-07-21 | 1971-09-02 | Carol Ann Franiel | Improvements in laminates |
CH526012A (de) * | 1970-04-07 | 1972-07-31 | Ver Drahtwerke Ag | Verfahren zur Herstellung von Nagelplatten und Einrichtung zur Durchführung des Verfahrens |
US3769142A (en) * | 1970-12-04 | 1973-10-30 | Mc Donnell Douglas Corp | Non-woven locked ply composite structure |
GB1411379A (en) * | 1971-12-21 | 1975-10-22 | Rolls Royce | Fibre reinforced composite structures |
US3837985A (en) * | 1972-02-24 | 1974-09-24 | Whittaker Corp | Multi-directional reinforced composite and method of making the same |
US4218276A (en) * | 1972-03-31 | 1980-08-19 | Avco Corporation | Method for making 3-D structures |
US4032383A (en) * | 1975-11-04 | 1977-06-28 | Mcdonnell Douglas Corporation | Fiber insertion device for continuous 3d foaming machine and method |
SU545483A2 (ru) * | 1975-12-24 | 1977-02-05 | Предприятие П/Я 7332 | Способ изготовлени силового элемента из стеклопластика |
DE2606666C2 (de) * | 1976-02-19 | 1982-03-18 | Greimbau-Lizenz-Gmbh, 3200 Hildesheim | Nagelplatte zum Verbinden von Holzbauteilen |
FR2433003A1 (fr) * | 1978-08-08 | 1980-03-07 | Commissariat Energie Atomique | Procede de fabrication d'un materiau renforce par une structure textile tridimensionnelle |
FR2446175A1 (fr) * | 1979-01-09 | 1980-08-08 | Europ Propulsion | Texture stratifiee renforcee |
US4350728A (en) * | 1980-10-02 | 1982-09-21 | The United States Of America As Represented By The Secretary Of The Navy | Cross reinforcement in a graphite-epoxy laminate |
-
1982
- 1982-12-17 DE DE19823246803 patent/DE3246803A1/de active Granted
-
1983
- 1983-11-30 US US06/556,704 patent/US4528051A/en not_active Expired - Fee Related
- 1983-12-12 GB GB08333128A patent/GB2132134B/en not_active Expired
- 1983-12-13 FR FR8319955A patent/FR2537916B1/fr not_active Expired
- 1983-12-15 ES ES528087A patent/ES8505583A1/es not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE3246803A1 (de) | 1984-06-20 |
GB2132134A (en) | 1984-07-04 |
GB2132134B (en) | 1986-12-10 |
US4528051A (en) | 1985-07-09 |
ES528087A0 (es) | 1985-06-01 |
ES8505583A1 (es) | 1985-06-01 |
FR2537916A1 (fr) | 1984-06-22 |
DE3246803C2 (es) | 1990-04-19 |
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ST | Notification of lapse |